US9573564B2 - Reel lock for passenger restraint having dual locking positions - Google Patents

Reel lock for passenger restraint having dual locking positions Download PDF

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Publication number
US9573564B2
US9573564B2 US13/595,354 US201213595354A US9573564B2 US 9573564 B2 US9573564 B2 US 9573564B2 US 201213595354 A US201213595354 A US 201213595354A US 9573564 B2 US9573564 B2 US 9573564B2
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locking
webbing
end plate
pawl
magnitude
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US20130134251A1 (en
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John Boyer
Daniel Meggs
Alan Lane
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Mission Systems Davenport Inc
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Carleton Life Support Systems Inc
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Assigned to CONAX FLORIDA CORPORATION reassignment CONAX FLORIDA CORPORATION ASSIGNMENT OF ASSIGNORS INTEREST (SEE DOCUMENT FOR DETAILS). Assignors: BOYER, JOHN, LANE, ALAN, MEGGS, DANIEL
Assigned to CARLETON LIFE SUPPORT SYSTEMS INC. reassignment CARLETON LIFE SUPPORT SYSTEMS INC. ASSIGNMENT OF ASSIGNORS INTEREST (SEE DOCUMENT FOR DETAILS). Assignors: CONAX FLORIDA CORPORATION
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Assigned to COBHAM MISSION SYSTEMS DAVENPORT LSS INC. reassignment COBHAM MISSION SYSTEMS DAVENPORT LSS INC. CHANGE OF NAME (SEE DOCUMENT FOR DETAILS). Assignors: CARLETON LIFE SUPPORT SYSTEMS INC.
Assigned to WILMINGTON TRUST, NATIONAL ASSOCIATION reassignment WILMINGTON TRUST, NATIONAL ASSOCIATION FIRST LIEN US INTELLECTUAL PROPERTY SECURITY AGREEMENT Assignors: CHELTON AVIONICS, INC., COBHAM ADVANCED ELECTRONIC SOLUTIONS INC., COBHAM MISSION SYSTEMS DAVENPORT AAR INC., COBHAM MISSION SYSTEMS DAVENPORT LSS INC., COBHAM MISSION SYSTEMS ORCHARD PARK INC.
Assigned to WILMINGTON TRUST, NATIONAL ASSOCIATION reassignment WILMINGTON TRUST, NATIONAL ASSOCIATION SECOND LIEN US INTELLECTUAL PROPERTY SECURITY AGREEMENT Assignors: CHELTON AVIONICS, INC., COBHAM ADVANCED ELECTRONIC SOLUTIONS INC., COBHAM MISSION SYSTEMS DAVENPORT AAR INC., COBHAM MISSION SYSTEMS DAVENPORT LSS INC., COBHAM MISSION SYSTEMS ORCHARD PARK INC.
Assigned to COBHAM MISSION SYSTEMS DAVENPORT AAR INC., COBHAM MISSION SYSTEMS DAVENPORT LSS INC., COBHAM MISSION SYSTEMS ORCHARD PARK INC. reassignment COBHAM MISSION SYSTEMS DAVENPORT AAR INC. PARTIAL RELEASE OF SECURITY INTEREST IN INTELLECTUAL PROPERTY Assignors: WILMINGTON TRUST, NATIONAL ASSOCIATION, AS SECURITY AGENT
Assigned to COBHAM MISSION SYSTEMS DAVENPORT AAR INC., COBHAM MISSION SYSTEMS DAVENPORT LSS INC., COBHAM MISSION SYSTEMS ORCHARD PARK INC. reassignment COBHAM MISSION SYSTEMS DAVENPORT AAR INC. PARTIAL RELEASE OF SECURITY INTEREST IN INTELLECTUAL PROPERTY Assignors: WILMINGTON TRUST, NATIONAL ASSOCIATION, AS SECURITY AGENT
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    • BPERFORMING OPERATIONS; TRANSPORTING
    • B60VEHICLES IN GENERAL
    • B60RVEHICLES, VEHICLE FITTINGS, OR VEHICLE PARTS, NOT OTHERWISE PROVIDED FOR
    • B60R22/00Safety belts or body harnesses in vehicles
    • B60R22/34Belt retractors, e.g. reels
    • B60R22/36Belt retractors, e.g. reels self-locking in an emergency
    • B60R22/38Belt retractors, e.g. reels self-locking in an emergency responsive only to belt movement
    • AHUMAN NECESSITIES
    • A62LIFE-SAVING; FIRE-FIGHTING
    • A62BDEVICES, APPARATUS OR METHODS FOR LIFE-SAVING
    • A62B1/00Devices for lowering persons from buildings or the like
    • A62B1/06Devices for lowering persons from buildings or the like by making use of rope-lowering devices
    • A62B1/08Devices for lowering persons from buildings or the like by making use of rope-lowering devices with brake mechanisms for the winches or pulleys
    • A62B1/10Devices for lowering persons from buildings or the like by making use of rope-lowering devices with brake mechanisms for the winches or pulleys mechanically operated
    • BPERFORMING OPERATIONS; TRANSPORTING
    • B60VEHICLES IN GENERAL
    • B60RVEHICLES, VEHICLE FITTINGS, OR VEHICLE PARTS, NOT OTHERWISE PROVIDED FOR
    • B60R22/00Safety belts or body harnesses in vehicles
    • B60R22/34Belt retractors, e.g. reels
    • B60R22/36Belt retractors, e.g. reels self-locking in an emergency
    • B60R22/38Belt retractors, e.g. reels self-locking in an emergency responsive only to belt movement
    • B60R2022/385Belt retractors, e.g. reels self-locking in an emergency responsive only to belt movement with adjustable sensitivity

Definitions

  • This invention relates to reel lock for use in conjunction with a passenger restraint system. More particularly, the present invention relates to a reel assembly with dual locking mechanisms, whereby an occupant can be restrained during both major and minor events.
  • U.S. Pat. No. 4,801,105 to Frisk discloses a reel assembly for retracting and locking a shoulder harness.
  • the assembly includes a strap supporting spool affixed to a ratchet wheel.
  • an inertia mass turns with respect to the reel. This causes the inertia mass to move forward axially and trip a dog which locks the reel.
  • U.S. Pat. No. 5,636,807 to Warrick discloses an acceleration sensor for an aircraft employing an inertia weight.
  • the inertia weight is movable within a chamber by way of a linkage.
  • the linkage is such that it provides the same output in response to movement of the aircraft in multiple directions.
  • FIG. 1 is a perspective view of the reel assembly of the present invention.
  • FIG. 2 is a cross sectional view illustrating the first locking mechanism of the reel assembly in the unlocked orientation.
  • FIG. 3 is a cross sectional view of the first locking mechanism of the reel assembly in the locked orientation.
  • FIG. 4 is a cross sectional view of the second locking mechanism of the reel assembly in the unlocked orientation.
  • FIG. 5 is a cross sectional view of the second locking mechanism of the reel assembly in the locked orientation.
  • FIG. 6 is a partially exploded view of the reel assembly showing both the first and second locking mechanisms.
  • FIG. 7 is a perspective cut away view of the first locking mechanism assembly in the unlocked orientation.
  • FIG. 8 is a perspective cut away view of the first locking mechanism in the locked orientation.
  • the present invention relates to an improved reel assembly for use in conjunction with the occupant restraint system of a vehicle.
  • the assembly employs a dual locking arrangement whereby an occupant can be restrained during both major and minor incidents. After a major incident, such as a collision, the reel assembly remains locked until the occupant disengages the reel by accessing a push button. After a minor incident, such as a fall, the reel assembly can be conveniently unlocked, without the need for accessing the push button, by applying counter tension to the restraint webbing.
  • Reel assembly 20 includes a housing 22 that contains a length of webbing 24 and associated locking and winding mechanisms. These mechanisms control the extraction and retraction of webbing 24 and are more fully described hereinafter.
  • An attachment 26 such as a clip, clasp or carabineer, can be attached to an end of webbing 24 and is used in securing webbing 24 to an occupant restraint, such as a waist belt or body harness.
  • Reel assembly 20 can be used in connection with any of a wide variety of vehicle restraint systems.
  • reel assembly 20 can be used in association with the aircrew restraint system disclosed in U.S. Pat. No. 7,275,710 to Van Druff et. al., the contents of which are incorporated herein by reference.
  • reel assembly 20 includes one or more mounting apertures for securing the assembly to the inside of an aircrew compartment. The reel can likewise be readily secured within other vehicles, such as automobiles or boats.
  • reel assembly 20 When used in connection with a restraint system, reel assembly 20 serves to restrain occupants during both major and minor incidents.
  • a “major incident” is generally defined as an event that results in more than 100 pounds of force being applied to webbing 24 .
  • a major incident for example, may occur when a harnessed aircrew member encounters a rapid change in altitude or excessive G forces.
  • a “minor incident” is generally defined as an event that results in less than 100 pounds of force being applied to webbing 24 .
  • a minor incident for example, may occur when a harnessed aircrew member trips or falls within the aircrew compartment.
  • Reel assembly 20 employs two distinct locking mechanisms for minor and major incidents.
  • the first locking mechanism which is actuated by major incidents, is illustrated in the cross-sectional views of FIGS. 2 and 3 .
  • the assembly includes shaft 28 about which webbing 24 can be wound or unwound.
  • Shaft 28 includes a geared end plate 32 .
  • end plate 32 is secured in facing relation with a peripheral locking ring 34 .
  • end plate 32 rotates together with locking ring 34 as webbing 24 is extracted and retracted from shaft 28 .
  • locking ring 34 is free to rotate independently of shaft 28 and end plate 32 . In other words, when forces greater than 100 pounds are applied to webbing 24 , locking ring 34 sides along the face of end plate 32 .
  • ring 34 and end plate 32 can be interconnected via a friction clutch that engages ring 34 and plate 32 during the less forceful extraction of webbing 24 .
  • Springs can also be used to provide a suitable interconnection.
  • One such interconnection is described in U.S. Pat. No. 4,955,556 to Frisk, the contents of which are incorporated by reference herein. Whichever of these mechanisms is employed, the rapid withdrawal of webbing 24 causes locking ring 34 to rotate slightly behind the rotation of shaft 28 .
  • the mechanism is such that the force necessary to cause the independent rotation of ring 34 is adjustable. In this manner, the threshhold necessary to trigger a major incident can be adjusted.
  • the first locking mechanism further includes a trigger 38 and an interconnected sear 52 that are positioned between ring 34 and shaft 28 .
  • Rotation of locking ring 34 relative to shaft 28 causes trigger 38 to engage an inclined ramp 36 on the inside face of ring 34 .
  • FIG. 6 illustrates trigger 38 engaging ramp 36 during the relative rotation of ring 34 .
  • Sear 52 is further interconnected to locking bolt 42 .
  • the movement of sear 52 permits locking bolt 42 to slide downwardly.
  • bolt 42 includes a cutout 44 and is encased within housing 46 .
  • bolt 42 is biased downwardly within housing 46 by spring 50 .
  • sear 52 is moved axially with respect to bolt 42 .
  • This permits bolt to move downwardly within housing 46 under bias of sprig 50 .
  • the sliding movement of bolt 42 triggers the pivotal movement of primary locking dog 48 . More specifically, as bolt 42 slides downwardly, a portion of locking dog 48 encounters the enlarged portion of cutout 44 . This, in turn, permits a spring to pivot locking dog 48 such that the distal end of the dog engages the teeth of geared end plate 32 .
  • webbing shaft 32 remains locked by way of locking dog 48 , thereby prohibiting rotation of shaft 28 and the further extraction of webbing 24 .
  • This serves to restrain the movement of an occupant within the associated harness.
  • Webbing shaft 28 remains locked until the occupant accesses and pushes button 54 .
  • button 54 By depressing button 54 , bolt 42 is slid upwardly, thereby disengaging locking dog 48 and trigger 38 .
  • the first locking mechanism is reset and webbing 24 can again be extracted or retracted as noted above.
  • FIGS. 4 and 5 illustrate a series of pawls 58 that are pivotally mounted upon the face of the geared end plate 32 . Although connected to plate 32 , the distal ends of pawls 58 are adapted to engage recesses 64 that are peripherally located about the inner circumference of locking ring 34 . Pawls 58 are maintained in a disengaged state by way of calibration springs 62 . These springs 62 are interconnected between the end plate 32 and the distal ends of pawls 58 .
  • the force of the springs is such that the pawls 58 are maintained in their disengaged orientation until a predetermined centripetal force is encountered (i.e. upon occurrence of a minor incident).
  • pawls 58 are pivoted outwardly to engage recesses 64 . This, in turn, will prevent rotation of shaft 28 and, thus, the further movement of the webbing 24 . In this orientation, the occupant is restrained.
  • pawls 58 can be reset by simply applying a counter tension to webbing 24 . Namely, by pulling back on webbing 24 the distal ends of pawls 58 will be removed from recesses 64 and, thereafter, springs 62 will serve to rotate pawls 58 back into the disengaged orientation. Webbing shaft 32 is then free to rotate and the occupant can move freely within the aircraft.
  • this implementation includes dual locking mechanisms for restraining a vehicle occupant by controlling the displacement of a length of webbing ( 24 ) during both major and minor incidents.
  • the webbing ( 24 ) includes a webbing clasp ( 26 ) at its distal end that can be releasably secured to a harness or other restraint system.
  • the webbing ( 24 ) is wound about a webbing shaft ( 28 ) within the interior of the reel assembly ( 20 ).
  • the shaft ( 28 ) includes a geared plate ( 32 ) at one end.
  • a sufficient length of webbing ( 24 ) is included so as to permit the restrained occupant to travel throughout the vehicle.
  • Rotation of the shaft ( 28 ) in a first sense results in the displacement of the webbing ( 24 ) and creation of sufficient slack so as to permit the free travel of the occupant within the vehicle.
  • rotation of the shaft ( 28 ) in the opposite sense results in slack being taken up so as to limit the movement of the occupant.
  • two distinct mechanisms are involved in preventing rotation of shaft ( 28 ). These mechanisms effectively restrain the occupant from any movement in the event the occupant falls (minor incident) or vehicle is involved in an accident (major incident).
  • FIGS. 4 and 5 a pair of locking pawls ( 58 ) are pivotally secured to the geared end plate ( 32 ).
  • FIG. 4 illustrates the pawls ( 58 ) in the unpivoted orientation
  • FIG. 5 illustrates the pawls ( 58 ) in the pivoted orientation.
  • a calibration spring ( 62 ) is secured to each locking pawl ( 58 ) and serves to bias the pawl ( 58 ) into the unpivoted orientation. The bias of these spring can be overcome by centripetal acceleration whenever the webbing shaft ( 28 ) is rotated at a predetermined rate. When such forces are encountered, the pawls ( 58 ) are forced outwardly to the pivoted orientation whereby at least one of the pawls ( 58 ) engages a surrounding locking ring ( 34 ) (note FIG. 5 ).
  • locking ring ( 34 ) includes a geared inner periphery that is adapted to be engaged by one of the pawls ( 58 ).
  • the locking ring ( 34 ) also includes an outer surface with an associated ramp ( 36 ) (note FIG. 6 ). The function of this ramp is described in greater detail hereinafter.
  • Locking ring ( 34 ) is positioned around the geared end plate ( 32 ) and is independently rotatable relative thereto. However, the locking ring ( 34 ) and the locking pawl ( 58 ) rotate together whenever one of the locking pawls ( 58 ) is engaged with the geared inner periphery of the locking ring ( 34 ). When this occurs, rotation of the webbing shaft ( 28 ) causes a corresponding rotation of the locking ring ( 34 ).
  • Spring compartments ( 40 ) and internal springs are included to resist the rotation of the locking ring ( 34 ).
  • Locking bolt ( 42 ) which includes an elongated cutout ( 44 ) along its length, is positioned adjacent the webbing shaft ( 28 ). Locking bolt ( 42 ) has both an engaged and a disengaged position. A spring ( 50 ) is used to bias the locking bolt ( 42 ) into the engaged position.
  • trigger ( 38 ) and a sear ( 52 ) are operatively coupled to the locking bolt ( 42 ) and operate to keep the locking bolt ( 42 ) in either its disengaged or its engaged orientation. More specifically, sear ( 52 ) engages the lower extent of locking bolt ( 42 ) and maintains it in the disengaged position against the bias of the spring ( 50 ).
  • trigger ( 38 ) is adapted to engage the ramp ( 36 ) on the outer surface of the locking ring ( 34 ) during the extended rotation of locking ring ( 34 ). Namely, trigger ( 38 ) engages ramp ( 36 ) whenever locking ring ( 34 ) is rotated more than 45 degrees.
  • both trigger ( 38 ) and sear ( 52 ) are pivoted such that sear ( 52 ) temporarily disengages the locking bolt ( 42 ).
  • This displacement of sear ( 52 ) permits spring ( 50 ) to force locking bolt ( 42 ) into the engaged position.
  • This movement of the locking bolt ( 42 ) permits a locking dog ( 48 ) to engage geared end plate ( 32 ) so as to prohibit further displacement of webbing ( 24 ).
  • the locking dog ( 48 ) is pivotally secured adjacent the geared end plate ( 32 ) and has a distal end that rides within the elongated cut out ( 44 ) of the locking bolt ( 42 ). As noted in FIG. 7 , the elongated cut out ( 44 ) prevents the locking dog ( 48 ) from engaging the geared end plate ( 32 ) when the locking bolt ( 42 ) is in the disengaged position. However, when the locking bolt ( 42 ) is in the engaged position, the geometry of the elongated cut out ( 44 ) allows the locking dog ( 48 ) to engage the geared end plate ( 32 ), as depicted in Figure B. With the locking dog ( 48 ) so engaged, the webbing ( 24 ) is prevented from being displaced from the webbing shaft ( 28 ) and the occupant is effectively restrained.
  • rotation of the webbing shaft ( 28 ) at a predetermined rate causes the locking pawls ( 58 ) to move into the pivoted orientation and engage the locking ring ( 34 ).
  • Locking pawls ( 58 ) remain engaged within locking ring ( 34 ) as long as tension remains in the webbing.
  • the locking pawls ( 58 ) can be disengaged by applying a counter tension to the webbing ( 24 ) to reset the assembly.
  • trigger ( 38 ) can also be tripped by a separate accelerometer ( 64 ).
  • This accelerometer ( 64 ) provides a separate and independent means of triggering locking dog ( 48 ) and preventing the rotation of webbing shaft ( 28 ) during major incidents.

Abstract

Disclosed is an improved reel assembly for use in conjunction with an occupant restraint system. The assembly employs a dual locking arrangement whereby an occupant can be restrained during both major and minor incidents. After a major incident, the reel assembly remains locked until the occupant disengages the reel via a push button. After a minor incident, the reel assembly can be conveniently unlocked, without the need for accessing the push button, by applying counter tension to the webbing.

Description

RELATED APPLICATION DATA
This application is a continuation of application Ser. No. 12/361,581 filed Jan. 29, 2009, and entitled “Reel Lock for Passenger Restraint Having Dual Locking Positions,” which itself claims priority to provisional application Ser. No. 61/024,409 filed on Jan. 29, 2008 and entitled “Reel Lock for Passenger Restraint Having Dual Locking Positions,” the contents of which are fully incorporated herein.
BACKGROUND OF THE INVENTION
Field of the Invention
This invention relates to reel lock for use in conjunction with a passenger restraint system. More particularly, the present invention relates to a reel assembly with dual locking mechanisms, whereby an occupant can be restrained during both major and minor events.
Description of the Background Art
The use of harness reels is known in the background art. For instance, U.S. Pat. No. 4,801,105 to Frisk discloses a reel assembly for retracting and locking a shoulder harness. The assembly includes a strap supporting spool affixed to a ratchet wheel. When a strap is rapidly pulled from the reel, an inertia mass turns with respect to the reel. This causes the inertia mass to move forward axially and trip a dog which locks the reel.
Likewise, U.S. Pat. No. 5,636,807 to Warrick discloses an acceleration sensor for an aircraft employing an inertia weight. The inertia weight is movable within a chamber by way of a linkage. The linkage is such that it provides the same output in response to movement of the aircraft in multiple directions.
Although these inventions each achieve their respective objectives, there continues to be a need in the art for a reel assembly with separate locking mechanisms that can be independently triggered and released in response to different events.
SUMMARY OF THE INVENTION
It is, therefore, one of the objects of this invention to provide a reel assembly with separate locking mechanisms.
It is another object of this invention to provide a reel with first and second locking mechanisms, wherein the first mechanism is triggered in response to major incidents and the second mechanism is triggered in response to minor incidents.
It is another object of the present invention to require a user to access a reset button to reset the reel after a major incident.
It is a further object of this invention to permit the reel assembly to be reset after a minor incident via the application of a counter tension to the harness webbing.
The foregoing has outlined rather broadly the more pertinent and important features of the present invention in order that the detailed description of the invention that follows may be better understood so that the present contribution to the art can be more fully appreciated. Additional features of the invention will be described hereinafter which form the subject of the claims of the invention. It should be appreciated by those skilled in the art that the conception and the specific embodiment disclosed may be readily utilized as a basis for modifying or designing other structures for carrying out the same purposes of the present invention. It should also be realized by those skilled in the art that such equivalent constructions do not depart from the spirit and scope of the invention as set forth in the appended claims.
BRIEF DESCRIPTION OF THE DRAWINGS
For a fuller understanding of the nature and objects of the invention, reference should be made to the following detailed description taken in connection with the accompanying drawings in which:
FIG. 1 is a perspective view of the reel assembly of the present invention.
FIG. 2 is a cross sectional view illustrating the first locking mechanism of the reel assembly in the unlocked orientation.
FIG. 3 is a cross sectional view of the first locking mechanism of the reel assembly in the locked orientation.
FIG. 4 is a cross sectional view of the second locking mechanism of the reel assembly in the unlocked orientation.
FIG. 5 is a cross sectional view of the second locking mechanism of the reel assembly in the locked orientation.
FIG. 6 is a partially exploded view of the reel assembly showing both the first and second locking mechanisms.
FIG. 7 is a perspective cut away view of the first locking mechanism assembly in the unlocked orientation.
FIG. 8 is a perspective cut away view of the first locking mechanism in the locked orientation.
Similar reference characters refer to similar parts throughout the several views of the drawings.
PARTS LIST
20 Reel Assembly 22 Reel Housing
24 Webbing 26 Webbing Clasp
28 Webbing Shaft 32 Geared End Plate of Webbing Shaft
34 Locking Ring 36 Ramp on Locking Ring
38 Trigger 40 Spring Housings
42 Locking Bolt 44 Cut Out in Locking Bolt
46 Housing for Locking Bolt 48 Primary Locking Dog
50 Locking Bolt Spring 52 Sear
54 Push Button 56 Guard
58 Pawls 62 Calibration Springs
64 Recesses on Locking Ring 66 Accelerometer
DETAILED DESCRIPTION OF THE PREFERRED EMBODIMENT
The present invention relates to an improved reel assembly for use in conjunction with the occupant restraint system of a vehicle. The assembly employs a dual locking arrangement whereby an occupant can be restrained during both major and minor incidents. After a major incident, such as a collision, the reel assembly remains locked until the occupant disengages the reel by accessing a push button. After a minor incident, such as a fall, the reel assembly can be conveniently unlocked, without the need for accessing the push button, by applying counter tension to the restraint webbing. The details of the present invention are more fully described hereinafter.
With reference now to FIG. 1, the improved reel assembly of the present invention is illustrated. Reel assembly 20 includes a housing 22 that contains a length of webbing 24 and associated locking and winding mechanisms. These mechanisms control the extraction and retraction of webbing 24 and are more fully described hereinafter. An attachment 26, such as a clip, clasp or carabineer, can be attached to an end of webbing 24 and is used in securing webbing 24 to an occupant restraint, such as a waist belt or body harness.
Reel assembly 20 can be used in connection with any of a wide variety of vehicle restraint systems. For instance, reel assembly 20 can be used in association with the aircrew restraint system disclosed in U.S. Pat. No. 7,275,710 to Van Druff et. al., the contents of which are incorporated herein by reference. In this regard, reel assembly 20 includes one or more mounting apertures for securing the assembly to the inside of an aircrew compartment. The reel can likewise be readily secured within other vehicles, such as automobiles or boats.
When used in connection with a restraint system, reel assembly 20 serves to restrain occupants during both major and minor incidents. A “major incident” is generally defined as an event that results in more than 100 pounds of force being applied to webbing 24. A major incident, for example, may occur when a harnessed aircrew member encounters a rapid change in altitude or excessive G forces. By contrast, a “minor incident” is generally defined as an event that results in less than 100 pounds of force being applied to webbing 24. A minor incident, for example, may occur when a harnessed aircrew member trips or falls within the aircrew compartment. Reel assembly 20 employs two distinct locking mechanisms for minor and major incidents.
The first locking mechanism, which is actuated by major incidents, is illustrated in the cross-sectional views of FIGS. 2 and 3. As illustrated, the assembly includes shaft 28 about which webbing 24 can be wound or unwound. Shaft 28 includes a geared end plate 32. As noted in FIGS. 4 and 5, end plate 32 is secured in facing relation with a peripheral locking ring 34. In the absence of a major incident, end plate 32 rotates together with locking ring 34 as webbing 24 is extracted and retracted from shaft 28. However, during a major incident, locking ring 34 is free to rotate independently of shaft 28 and end plate 32. In other words, when forces greater than 100 pounds are applied to webbing 24, locking ring 34 sides along the face of end plate 32. In this regard, ring 34 and end plate 32 can be interconnected via a friction clutch that engages ring 34 and plate 32 during the less forceful extraction of webbing 24. Springs can also be used to provide a suitable interconnection. One such interconnection is described in U.S. Pat. No. 4,955,556 to Frisk, the contents of which are incorporated by reference herein. Whichever of these mechanisms is employed, the rapid withdrawal of webbing 24 causes locking ring 34 to rotate slightly behind the rotation of shaft 28. Ideally, the mechanism is such that the force necessary to cause the independent rotation of ring 34 is adjustable. In this manner, the threshhold necessary to trigger a major incident can be adjusted.
The first locking mechanism further includes a trigger 38 and an interconnected sear 52 that are positioned between ring 34 and shaft 28. Rotation of locking ring 34 relative to shaft 28 causes trigger 38 to engage an inclined ramp 36 on the inside face of ring 34. FIG. 6 illustrates trigger 38 engaging ramp 36 during the relative rotation of ring 34. This, in turn, results in the movement of both trigger 38 and an interconnected sear 52 in a direction parallel to the length of housing 20. Sear 52 is further interconnected to locking bolt 42. The movement of sear 52 permits locking bolt 42 to slide downwardly. As illustrated in FIGS. 7 and 8, bolt 42 includes a cutout 44 and is encased within housing 46.
With continuing reference FIGS. 7 and 8, bolt 42 is biased downwardly within housing 46 by spring 50. Thus, during a major incident, as trigger 38 engages ramp 40, sear 52 is moved axially with respect to bolt 42. This, in turn, permits bolt to move downwardly within housing 46 under bias of sprig 50. The sliding movement of bolt 42 triggers the pivotal movement of primary locking dog 48. More specifically, as bolt 42 slides downwardly, a portion of locking dog 48 encounters the enlarged portion of cutout 44. This, in turn, permits a spring to pivot locking dog 48 such that the distal end of the dog engages the teeth of geared end plate 32.
As further noted in FIGS. 7 and 8, the downward movement of bolt 42 also results in push button 54 being accessible within guard housing 56. Thus, after the occurrence of a major incident, webbing shaft 32 remains locked by way of locking dog 48, thereby prohibiting rotation of shaft 28 and the further extraction of webbing 24. This serves to restrain the movement of an occupant within the associated harness. Webbing shaft 28 remains locked until the occupant accesses and pushes button 54. By depressing button 54, bolt 42 is slid upwardly, thereby disengaging locking dog 48 and trigger 38. As a result, the first locking mechanism is reset and webbing 24 can again be extracted or retracted as noted above.
The second locking mechanism, which is activated by minor incidents, is described next in conjunction with FIGS. 4 and 5. These figures illustrate a series of pawls 58 that are pivotally mounted upon the face of the geared end plate 32. Although connected to plate 32, the distal ends of pawls 58 are adapted to engage recesses 64 that are peripherally located about the inner circumference of locking ring 34. Pawls 58 are maintained in a disengaged state by way of calibration springs 62. These springs 62 are interconnected between the end plate 32 and the distal ends of pawls 58. The force of the springs is such that the pawls 58 are maintained in their disengaged orientation until a predetermined centripetal force is encountered (i.e. upon occurrence of a minor incident). When such a force is encountered, pawls 58 are pivoted outwardly to engage recesses 64. This, in turn, will prevent rotation of shaft 28 and, thus, the further movement of the webbing 24. In this orientation, the occupant is restrained.
After the occurrence of a minor incident, pawls 58 can be reset by simply applying a counter tension to webbing 24. Namely, by pulling back on webbing 24 the distal ends of pawls 58 will be removed from recesses 64 and, thereafter, springs 62 will serve to rotate pawls 58 back into the disengaged orientation. Webbing shaft 32 is then free to rotate and the occupant can move freely within the aircraft.
Alternative Embodiment
A specific implementation of the present invention is next described in conjunction with FIGS. 1-8. As with the primary embodiment, this implementation includes dual locking mechanisms for restraining a vehicle occupant by controlling the displacement of a length of webbing (24) during both major and minor incidents. As is conventional, the webbing (24) includes a webbing clasp (26) at its distal end that can be releasably secured to a harness or other restraint system.
The webbing (24) is wound about a webbing shaft (28) within the interior of the reel assembly (20). As illustrated in FIG. 2, the shaft (28) includes a geared plate (32) at one end. A sufficient length of webbing (24) is included so as to permit the restrained occupant to travel throughout the vehicle. Rotation of the shaft (28) in a first sense results in the displacement of the webbing (24) and creation of sufficient slack so as to permit the free travel of the occupant within the vehicle. Likewise, rotation of the shaft (28) in the opposite sense results in slack being taken up so as to limit the movement of the occupant. As described in greater detail hereinafter, two distinct mechanisms are involved in preventing rotation of shaft (28). These mechanisms effectively restrain the occupant from any movement in the event the occupant falls (minor incident) or vehicle is involved in an accident (major incident).
As illustrated in FIGS. 4 and 5, a pair of locking pawls (58) are pivotally secured to the geared end plate (32). FIG. 4 illustrates the pawls (58) in the unpivoted orientation and FIG. 5 illustrates the pawls (58) in the pivoted orientation. A calibration spring (62) is secured to each locking pawl (58) and serves to bias the pawl (58) into the unpivoted orientation. The bias of these spring can be overcome by centripetal acceleration whenever the webbing shaft (28) is rotated at a predetermined rate. When such forces are encountered, the pawls (58) are forced outwardly to the pivoted orientation whereby at least one of the pawls (58) engages a surrounding locking ring (34) (note FIG. 5).
As illustrated, locking ring (34) includes a geared inner periphery that is adapted to be engaged by one of the pawls (58). The locking ring (34) also includes an outer surface with an associated ramp (36) (note FIG. 6). The function of this ramp is described in greater detail hereinafter. Locking ring (34) is positioned around the geared end plate (32) and is independently rotatable relative thereto. However, the locking ring (34) and the locking pawl (58) rotate together whenever one of the locking pawls (58) is engaged with the geared inner periphery of the locking ring (34). When this occurs, rotation of the webbing shaft (28) causes a corresponding rotation of the locking ring (34). Spring compartments (40) and internal springs are included to resist the rotation of the locking ring (34).
The operation of the locking bolt (42) is described next in association with FIGS. 7 and 8. Locking bolt (42), which includes an elongated cutout (44) along its length, is positioned adjacent the webbing shaft (28). Locking bolt (42) has both an engaged and a disengaged position. A spring (50) is used to bias the locking bolt (42) into the engaged position. With continuing reference to FIGS. 7 and 8, trigger (38) and a sear (52) are operatively coupled to the locking bolt (42) and operate to keep the locking bolt (42) in either its disengaged or its engaged orientation. More specifically, sear (52) engages the lower extent of locking bolt (42) and maintains it in the disengaged position against the bias of the spring (50).
With reference to FIG. 6, it can be seen that trigger (38) is adapted to engage the ramp (36) on the outer surface of the locking ring (34) during the extended rotation of locking ring (34). Namely, trigger (38) engages ramp (36) whenever locking ring (34) is rotated more than 45 degrees. When this occurs, both trigger (38) and sear (52) are pivoted such that sear (52) temporarily disengages the locking bolt (42). This displacement of sear (52) permits spring (50) to force locking bolt (42) into the engaged position. This movement of the locking bolt (42), in turn, permits a locking dog (48) to engage geared end plate (32) so as to prohibit further displacement of webbing (24).
The locking dog (48) is pivotally secured adjacent the geared end plate (32) and has a distal end that rides within the elongated cut out (44) of the locking bolt (42). As noted in FIG. 7, the elongated cut out (44) prevents the locking dog (48) from engaging the geared end plate (32) when the locking bolt (42) is in the disengaged position. However, when the locking bolt (42) is in the engaged position, the geometry of the elongated cut out (44) allows the locking dog (48) to engage the geared end plate (32), as depicted in Figure B. With the locking dog (48) so engaged, the webbing (24) is prevented from being displaced from the webbing shaft (28) and the occupant is effectively restrained.
In operation, rotation of the webbing shaft (28) at a predetermined rate causes the locking pawls (58) to move into the pivoted orientation and engage the locking ring (34). This restricts the displacement of the webbing (24) from the webbing shaft (28) and restrains the occupant. This level of restraint is triggered during minor incidents, such as when the occupant trips or falls. Locking pawls (58) remain engaged within locking ring (34) as long as tension remains in the webbing. The locking pawls (58) can be disengaged by applying a counter tension to the webbing (24) to reset the assembly.
During major incidents, such a vehicle accident, the force on the webbing (24) will cause the locking pawls (58) to engage locking ring (34) and will further cause the locking ring (34) to rotate 450 or more. This rotation, in turn, causes trigger (38) to engage ramp (36), whereby sear (52) will be displaced. As noted in FIG. 8, spring (50) will thereafter be permitted to move the locking bolt (42) into the engaged position such that the locking dog (48) engages the geared end plate (32). With the locking dog (48) fully engaged, further displacement of the webbing (24) is prevented and the occupant is fully restrained. Thus, during major incidents, an occupant is fully restrained. The user can thereafter release the locking dog (48) via a push button at the end of locking bolt (42). In addition to the foregoing, trigger (38) can also be tripped by a separate accelerometer (64). This accelerometer (64) provides a separate and independent means of triggering locking dog (48) and preventing the rotation of webbing shaft (28) during major incidents.
The present disclosure includes that contained in the appended claims, as well as that of the foregoing description. Although this invention has been described in its preferred form with a certain degree of particularity, it is understood that the present disclosure of the preferred form has been made only by way of example and that numerous changes in the details of construction and the combination and arrangement of parts may be resorted to without departing from the spirit and scope of the invention.

Claims (11)

What is claimed is:
1. A reel assembly (20) for controlling the displacement of webbing (24) comprising:
a webbing shaft (28) with a geared end plate (32) rotatably mounted within a housing, the webbing (24) being wound about the webbing shaft (28), with displacement of the webbing (24) being controlled by rotation of the webbing shaft (28);
at least one locking pawl (58) pivotally secured to the geared end plate (32), the at least one locking pawl (58) having pivoted and unpivoted orientations, a calibration spring (62) secured to a respective locking pawl (58), the calibration spring (62) having a bias that functions to urge the respective pawl (58) into the unpivoted orientation, the bias being overcome when a force having a first magnitude is applied to the webbing shaft (28), whereby the respective pawl (58) is moved to the pivoted orientation; and
a locking ring (34) having a geared inner periphery, the locking ring (34) positioned around and independently rotatable relative to the geared end plate (32), the respective locking pawl (58) engaging the geared inner periphery of the locking ring (34) when the respective pawl (58) is in the pivoted orientation, whereby when the force having the first magnitude is applied to the webbing shaft, rotation of the webbing shaft (28) is arrested solely by the engagement of the respective locking pawl (58) with the inner periphery of the locking ring (34); and
a locking dog (48) that lockingly engages the geared end plate (32) to prevent displacement of the webbing (24) upon independent rotation of the locking ring (34) when a force having a second magnitude is applied to the webbing shaft, wherein the second magnitude is greater than the first magnitude.
2. The reel assembly as described in claim 1 further comprising:
a locking bolt (42) positioned adjacent the webbing shaft (28), the locking bolt (42) having engaged and disengaged positions, with the webbing (24) prevented from displacement with the locking bolt (42) in the engaged position.
3. The reel assembly as described in claim 2 further comprising:
a trigger (38) for bringing the locking bolt (42) into the engaged position upon independent rotation of the locking ring (34) when a force having a second magnitude is applied to the webbing shaft.
4. The reel assembly as described in claim 3 further comprising:
a locking dog (48) that is pivotally secured adjacent the geared end plate (32), the locking dog (48) disengaged from the geared end plate (32) when the locking bolt (42) is in the disengaged position and the locking dog (48) engaged with the geared end plate (32) when the locking bolt is in the engaged position, with the locking dog (48) in engagement with the geared end plate (32) the webbing (24) is prevented from being displaced from the webbing shaft (28).
5. The reel assembly as described in claim 4 wherein locking bolt (42) includes an elongated cut out (44) and wherein the locking dog (48) includes a distal end that rides within the elongated cut out (44), whereby the geometry of the elongated cut out (44) forces the locking dog (48) into engagement with the geared end plate (32) when the locking bolt is in the engaged position.
6. The reel assembly as described in claim 3 further comprising an accelerometer that can engage the trigger (38) upon application of the force having the second magnitude.
7. A reel assembly (20) for controlling the displacement of webbing (24) comprising:
a webbing shaft (28) with an end plate (32) rotatably mounted within a housing, the webbing (24) being wound about the webbing shaft (28);
a pawl (58) pivotally secured to the end plate (32), the pawl (58) having locked and unlocked orientations, the pawl (58) being brought to the locked orientation when a force having a first magnitude is applied to the webbing shaft (28);
a locking ring (34) having an inner periphery, the locking ring (34) positioned around and independently rotatable relative to the end plate (32), whereby when the force having the first magnitude is applied to the webbing shaft, rotation of the webbing shaft (28) is arrested solely by engagement of the pawl (58) with the inner periphery of the locking ring (34); and
a locking dog (48) that lockingly engages the geared end plate (32) to prevent displacement of the webbing (24) upon rotation of locking ring (34) when a force having a second magnitude is applied to the webbing shaft,
wherein in the second magnitude is greater than the first magnitude.
8. The reel assembly (20) as described in claim 7 wherein both the end plate (32) and the locking ring (34) are geared.
9. The reel assembly (20) as described in claim 7 wherein the end plate (32) and locking ring (34) rotate independently of one another when the force having the second magnitude is applied to the webbing shaft.
10. The reel assembly (20) as described in claim 7 further comprising a calibration spring (62) secured to the pawl (58), the calibration spring (62) having a bias that functions to urge the pawl (58) into the unlocked orientation, the bias being overcome when the force having the first magnitude is applied to the webbing shaft (28), whereby the pawl (58) is moved to the locked orientation.
11. The reel assembly (20) as described in claim 7 further comprising an accelerometer that is used in triggering the locking dog (48).
US13/595,354 2008-01-29 2012-08-27 Reel lock for passenger restraint having dual locking positions Active US9573564B2 (en)

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US2440908P 2008-01-29 2008-01-29
US12/361,581 US8251304B2 (en) 2008-01-29 2009-01-29 Reel lock for passenger restraint having dual locking positions
US13/595,354 US9573564B2 (en) 2008-01-29 2012-08-27 Reel lock for passenger restraint having dual locking positions

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Cited By (1)

* Cited by examiner, † Cited by third party
Publication number Priority date Publication date Assignee Title
US20200078621A1 (en) * 2018-09-11 2020-03-12 Yoke Industrial Corp. Fall arrest device

Families Citing this family (14)

* Cited by examiner, † Cited by third party
Publication number Priority date Publication date Assignee Title
WO2012018788A1 (en) 2010-08-02 2012-02-09 Conax Florida Corporation Restraint and extraction harness with associated release mechanism
US8516979B2 (en) * 2010-09-27 2013-08-27 Joseph Ek Retractable leash with automatic braking mechanism
US8662436B2 (en) * 2010-12-23 2014-03-04 Carleton Life Support Systems Inc. Apparatus for adjusting the payout of tether from a reel assembly
US8612099B2 (en) * 2011-05-06 2013-12-17 Tk Holdings Inc. Occupant restraint system
US9144720B1 (en) * 2014-06-18 2015-09-29 Wilson Sporting Goods Co. Golf club adjustable hosel assembly
US9144719B1 (en) * 2014-06-18 2015-09-29 Wilson Sporting Goods Co. Golf club adjustable hosel assembly
US9358429B2 (en) * 2014-06-18 2016-06-07 Wilson Sporting Goods Co. Golf club adjustable hosel assembly
US9517841B2 (en) 2015-04-01 2016-12-13 Carleton Life Support Systems, Inc. Ballistic powered inertia reel
DE102015109444B4 (en) * 2015-06-12 2018-08-02 Bornack Gmbh & Co. Kg Rope securing device
US9751495B2 (en) * 2015-08-21 2017-09-05 Carleton Life Support Systems, Inc. Reel lock having multiple tooth dog
FR3042718B1 (en) * 2015-10-26 2017-12-01 Vertic AUTOMATICALLY RECALLING FALL ARREST
MX2018007331A (en) * 2015-12-18 2019-01-10 Eddy Current Lp A variable behaviour control mechanism for a motive system.
USD929074S1 (en) * 2018-04-05 2021-08-31 Braunability Uk Limited Safety belt
US11833994B1 (en) 2021-11-29 2023-12-05 Clinton A. Sadler Pet safety restraint device for vehicles

Citations (22)

* Cited by examiner, † Cited by third party
Publication number Priority date Publication date Assignee Title
US2791397A (en) * 1954-11-24 1957-05-07 Inland Steel Co Safety reel
US3240510A (en) * 1962-06-13 1966-03-15 Pacific Scientific Co Safety harness
US4083511A (en) * 1975-04-03 1978-04-11 Nsk-Warner K. K. Seat belt retractor
US4193564A (en) * 1978-05-03 1980-03-18 Lindblad S M Locking device in connection with safety belts
US4381086A (en) * 1980-09-25 1983-04-26 Allied Corporation Seat belt retractor structure
US4386745A (en) * 1981-08-10 1983-06-07 General Motors Corporation Tension reliever for seat belt retractor
US4396167A (en) * 1981-04-08 1983-08-02 General Motors Corporation Lock bar and belt clamp release for seat belt retractor
US4401282A (en) * 1980-08-19 1983-08-30 Nissan Motor Co., Ltd. Emergency locking seat belt retractor
US4422594A (en) * 1980-11-14 1983-12-27 Repa Feinstanzwerk Gmbh Automatic roll-up device for a safety belt
US4801105A (en) * 1987-10-01 1989-01-31 Pzf, Inc. Shoulder harness reel assembly with automatic reel lock
US4917325A (en) * 1987-12-23 1990-04-17 Allied-Signal Inc. Webbing sensor
US4925124A (en) * 1987-04-03 1990-05-15 Pacific Scientific Company Dual-mode inertia reel system
US5127598A (en) * 1989-09-11 1992-07-07 Takata Corporation Seat belt retractor
US5351906A (en) * 1990-12-21 1994-10-04 Barrow Hepburn Sala Ltd. Safety anchorages for controlling pay-out of a safety line
US5522564A (en) * 1993-09-13 1996-06-04 Autoliv Development Ab Safety belt reeling device and safety belt tightening device combination with power limiter
US5524833A (en) * 1993-10-04 1996-06-11 Trw Repa Gmbh Seat belt retractor
US5526996A (en) * 1993-05-05 1996-06-18 Trw Repa Gmbh Seat belt retractor
US5636807A (en) * 1994-08-01 1997-06-10 H. Koch & Sons Co., Inc. Acceleration sensor having inertia weight responsive to accelerations in every direction
US5771993A (en) * 1996-06-14 1998-06-30 Dalloz Safety, Inc. Safety devices for fall restraint
US5921496A (en) * 1995-03-16 1999-07-13 Nsk Ltd. Retractor for use with a seat belt
EP1714843A1 (en) 2005-04-22 2006-10-25 Key Safety Systems, Inc. Seat belt retractor with improved web sensor
US20060284012A1 (en) * 2005-06-15 2006-12-21 Vandruff Charles E Aircrew restraint system

Family Cites Families (1)

* Cited by examiner, † Cited by third party
Publication number Priority date Publication date Assignee Title
US4955556A (en) 1987-10-01 1990-09-11 Pzf, Inc. Shoulder harness reel assembly with automatic reel lock

Patent Citations (23)

* Cited by examiner, † Cited by third party
Publication number Priority date Publication date Assignee Title
US2791397A (en) * 1954-11-24 1957-05-07 Inland Steel Co Safety reel
US3240510A (en) * 1962-06-13 1966-03-15 Pacific Scientific Co Safety harness
US4083511A (en) * 1975-04-03 1978-04-11 Nsk-Warner K. K. Seat belt retractor
US4193564A (en) * 1978-05-03 1980-03-18 Lindblad S M Locking device in connection with safety belts
US4401282A (en) * 1980-08-19 1983-08-30 Nissan Motor Co., Ltd. Emergency locking seat belt retractor
US4381086A (en) * 1980-09-25 1983-04-26 Allied Corporation Seat belt retractor structure
US4422594A (en) * 1980-11-14 1983-12-27 Repa Feinstanzwerk Gmbh Automatic roll-up device for a safety belt
US4396167A (en) * 1981-04-08 1983-08-02 General Motors Corporation Lock bar and belt clamp release for seat belt retractor
US4386745A (en) * 1981-08-10 1983-06-07 General Motors Corporation Tension reliever for seat belt retractor
US4925124A (en) * 1987-04-03 1990-05-15 Pacific Scientific Company Dual-mode inertia reel system
US4801105A (en) * 1987-10-01 1989-01-31 Pzf, Inc. Shoulder harness reel assembly with automatic reel lock
US4917325A (en) * 1987-12-23 1990-04-17 Allied-Signal Inc. Webbing sensor
US5127598A (en) * 1989-09-11 1992-07-07 Takata Corporation Seat belt retractor
US5351906A (en) * 1990-12-21 1994-10-04 Barrow Hepburn Sala Ltd. Safety anchorages for controlling pay-out of a safety line
US5526996A (en) * 1993-05-05 1996-06-18 Trw Repa Gmbh Seat belt retractor
US5522564A (en) * 1993-09-13 1996-06-04 Autoliv Development Ab Safety belt reeling device and safety belt tightening device combination with power limiter
US5524833A (en) * 1993-10-04 1996-06-11 Trw Repa Gmbh Seat belt retractor
US5636807A (en) * 1994-08-01 1997-06-10 H. Koch & Sons Co., Inc. Acceleration sensor having inertia weight responsive to accelerations in every direction
US5921496A (en) * 1995-03-16 1999-07-13 Nsk Ltd. Retractor for use with a seat belt
US5771993A (en) * 1996-06-14 1998-06-30 Dalloz Safety, Inc. Safety devices for fall restraint
EP1714843A1 (en) 2005-04-22 2006-10-25 Key Safety Systems, Inc. Seat belt retractor with improved web sensor
US20060237573A1 (en) * 2005-04-22 2006-10-26 Key Safety Systems, Inc. Seat belt retractor with improved web sensor
US20060284012A1 (en) * 2005-06-15 2006-12-21 Vandruff Charles E Aircrew restraint system

Cited By (2)

* Cited by examiner, † Cited by third party
Publication number Priority date Publication date Assignee Title
US20200078621A1 (en) * 2018-09-11 2020-03-12 Yoke Industrial Corp. Fall arrest device
US10960243B2 (en) * 2018-09-11 2021-03-30 Yoke Industrial Corp. Fall arrest device

Also Published As

Publication number Publication date
US20090321550A1 (en) 2009-12-31
EP2242543A1 (en) 2010-10-27
EP3002047A1 (en) 2016-04-06
EP3002046B1 (en) 2017-08-16
EP2242543B1 (en) 2017-07-26
US8251304B2 (en) 2012-08-28
EP3002047B1 (en) 2017-04-26
US20130134251A1 (en) 2013-05-30
EP2242543A4 (en) 2016-01-20
EP3002046A1 (en) 2016-04-06
WO2009097376A1 (en) 2009-08-06

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